Based on upwind differencing of the governing equations, inherent diss
ipation terms are derived for three-dimensional hyperbolic grid genera
tion, These terms, taking only a negligible amount of mathematic opera
tions, can effectively eliminate grid oscillation that is often encoun
tered in hyperbolic grid generation, In addition to these dissipation
terms, a Laplacian-type smoothing is incorporated to increase smoothne
ss. Both implicit and explicit schemes for three-dimensional hyperboli
c grid generation are investigated, and a comparison of these two sche
mes is made, Several different geometries are used to demonstrate the
robustness of the new methods, Finally, a wing-body configuration, wit
h severe concave and convex corners, is used to evaluate the versatili
ty of the present methods.